Mission type | Optical imaging reconnaissance |
---|---|
Operator | OKB-1 |
COSPAR ID | 1966-037A |
SATCAT no. | 02163 |
Mission duration | 8 days |
Spacecraft properties | |
Spacecraft type | Zenit-2 |
Manufacturer | OKB-1 |
Launch mass | 4730 kg[1] |
Start of mission | |
Launch date | 6 May 1966, 11:02:00 GMT[2] |
Rocket | Vostok-2 s/n N15001-01 |
Launch site | Baikonur, Site 31/6 |
Contractor | OKB-1 |
End of mission | |
Disposal | Recovered |
Landing date | 14 May 1966, 08:24 GMT[3] |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Low Earth |
Perigee altitude | 205 km |
Apogee altitude | 298 km |
Inclination | 65.0° |
Period | 89.5 minutes |
Epoch | 6 May 1966 |
Kosmos 117 (Russian: Космос 117 meaning Cosmos 117) or Zenit-2 No.39 was a Soviet optical film-return reconnaissance satellite launched in 1966. A Zenit-2 spacecraft, Kosmos 117 was the thirty-eighth of eighty-one such satellites to be launched[4][5] and had a mass of 4,730 kilograms (10,430 lb).
Kosmos 117 was launched by a Vostok-2 rocket, serial number N15001-01,[6] flying from Site 31/6 at the Baikonur Cosmodrome. The launch took place at 11:02 GMT on 6 May 1966, and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1966-037A and the Satellite Catalog Number 02163.[1]
Kosmos 117 was operated in a low Earth orbit, at an epoch of 6 May 1966, it had a perigee of 205 kilometres (127 mi), an apogee of 298 kilometres (185 mi), an inclination of 65.0°, and an orbital period of 89.5 minutes.[2] After eight days in orbit, Kosmos 117 was deorbited, with its return capsule descending under parachute and landing at 08:24 GMT on 14 May 1966 and recovered by Soviet force.[3]